Attitude tracking control for rigid-flexible coupled spacecraft with guaranteed performance bounds

Yan Xiao; Anton H.J. de Ruiter; Dong Ye; Zhaowei Sun

doi:10.2514/1.G004535

Attitude tracking control for rigid-flexible coupled spacecraft with guaranteed performance bounds

Yan Xiao
, Anton H.J. de Ruiter
, Dong Ye^*
, Zhaowei Sun

^*Corresponding author for this work

School of Astronautics

Research Center of Satellite Technology
Toronto Metropolitan University

Research output: Contribution to journal › Article › peer-review

19 Scopus citations

Original language	English
Pages (from-to)	327-337
Number of pages	11
Journal	Journal of Guidance, Control, and Dynamics
Volume	43
Issue number	2
DOIs	https://doi.org/10.2514/1.G004535
State	Published - 2020

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10.2514/1.G004535

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title = "Attitude tracking control for rigid-flexible coupled spacecraft with guaranteed performance bounds",

author = "Yan Xiao and \{de Ruiter\}, \{Anton H.J.\} and Dong Ye and Zhaowei Sun",

year = "2020",

doi = "10.2514/1.G004535",

language = "英语",

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issn = "0731-5090",

publisher = "American Institute of Aeronautics and Astronautics Inc. (AIAA)",

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TY - JOUR

T1 - Attitude tracking control for rigid-flexible coupled spacecraft with guaranteed performance bounds

AU - Xiao, Yan

AU - de Ruiter, Anton H.J.

AU - Ye, Dong

AU - Sun, Zhaowei

PY - 2020

Y1 - 2020

UR - https://www.scopus.com/pages/publications/85078119785

U2 - 10.2514/1.G004535

DO - 10.2514/1.G004535

M3 - 文章

AN - SCOPUS:85078119785

SN - 0731-5090

VL - 43

SP - 327

EP - 337

JO - Journal of Guidance, Control, and Dynamics

JF - Journal of Guidance, Control, and Dynamics

IS - 2

ER -

Attitude tracking control for rigid-flexible coupled spacecraft with guaranteed performance bounds

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